Airworthiness Directive 2019-19-13

one-time
Official AD 2019-19-13 · FR doc 2019-22567 · 2019-10-21 · airframe

Airworthiness Directives; Airbus Helicopters

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for certain Airbus Helicopters Model EC225LP helicopters. This AD requires determining the total hours time-in-service (TIS) of the free wheel shafts of certain main rotor gearboxes (MGBs), replacing the MGB or right-hand side (RH) free wheel shaft, installing placard(s), and revising the Rotorcraft Flight Manual (RFM) for your helicopter. This AD was prompted by a report of wear of the ramps of the RH free wheel shaft. The actions of this AD are intended to address an unsafe condition on these products.

Which aircraft AD 2019-19-13 applies to

MakesAirbus Helicopters
ModelsEC225LP, EC225
Part-conditional332A325001.XX, 332A325002.XX, 332A325003.XX, 332A325011.XX, 332A325012.XX, 332A325013.XX, 332A322191.20.

Applies to helicopters with a main rotor gearbox (MGB) P/N 332A325001.XX, .002.XX, or .003.XX, with a main reduction gear module (with MOD 07-53016, i.e., 16-roller free wheel of free wheel shaft P/N 332A322191.20) installed, P/N 332A325011.XX, .012.XX, or .013.XX, where 'XX' denotes any dash number.

Whether AD 2019-19-13 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

How AD compliance is recorded

A valid compliance record (14 CFR 43.9) states:

Method of complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 2019-19-13 complied with on your aircraft?

Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.

Look up a tail number →Read the full directive (Federal Register)

Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.